摘要
为了对设计初期或国外的等数据不足的飞机进行六自由度仿真,根据等效系统的思路,建立了等效力矩导数模型,提供了等效力矩导数的计算过程。验证表明,等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
To realize the 6-DOF simulation of the aircraft without full moment derivatives, such as the aircraft in preparatory design process or the foreign aircraft, an equivalent moment derivatives model is presented on the thinking about an equivalent system. The derivation of equivalent moment derivatives is presented. Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
出处
《飞行力学》
CSCD
北大核心
2006年第4期14-17,共4页
Flight Dynamics
关键词
等效力矩导数
动力学
飞行仿真
equivalent moment derivatives
dynamies
flight simulation
